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Testing of a Loop Heat Pipe Subjected to Variable Accelerating ForcesThis paper presents viewgraphs of the functionality of a loop heat pipe that was subjected to variable accelerating forces. The topics include: 1) Summary of LHP (Loop Heat Pipe) Design Parameters; 2) Picture of the LHP; 3) Schematic of Test Setup; 4) Test Configurations; 5) Test Profiles; 6) Overview of Test Results; 7) Start-up; 8) Typical Start-up without Temperature Overshoot; 9) Start-up with a Large Temperature Overshoot; 10) LHP Operation Under Stationary Condition; 11) LHP Operation Under Continuous Acceleration; 12) LHP Operation Under Periodic Acceleration; 13) Effects of Acceleration on Temperature Oscillation and Hysteresis; 14) Temperature Oscillation/Hysteresis vs Spin Rate; and 15) Summary.
Document ID
20000032958
Acquisition Source
Goddard Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Ku, Jentung
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Ottenstein, Laura
(NASA Goddard Space Flight Center Greenbelt, MD United States)
Kaya, Tarik
(ISU Greenbelt, MD United States)
Rogers, Paul
(Army Tank-Automotive Research and Development Command Warren, MI United States)
Hoff, Craig
(Kettering Univ. Flint, MI United States)
Date Acquired
September 7, 2013
Publication Date
January 1, 2000
Subject Category
Fluid Mechanics And Thermodynamics
Meeting Information
Meeting: 11th Annual Spacecraft Themal Control Technology Workshop
Location: El Segundo, CA
Country: United States
Start Date: March 1, 2000
End Date: March 3, 2000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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